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DTIC AD0804527: JTF17A-21B TURBOFAN ENGINE SPECIFICATION

by: Defense Technical Information Center

Publication date: 1966-08-08

Collection: dticarchive; additional_collections

Language: English

This specification establishes design and performance requirements for the Pratt and Whitney Aircraft JTF17A-21B turbofan engine to be certificated in Phase 4 of the Supersonic Transport Program. Significant differences in the design and performance of the Phase 3 Flight Test Status engines for airplane flight testing are noted.

Addeddate: 2019-12-03 23:16:20

Foldoutcount: 0

Identifier: DTIC_AD0804527

Identifier-ark: ark:/13960/t0dv9nk1h

Ocr_converted: abbyy-to-hocr 1.1.37

Ocr_module_version: 0.0.21

Page_number_confidence: 46

Page_number_module_version: 1.0.3

Pages: 96

Ppi: 300

Year: 1966

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